A flow visualization study was performed using a focusing schlieren system in the 0.3m Transonic Cryogenic Tunnel at NASA Langley Research Center. The design employed proved to be a useful flow visualization tool for flows as low as M = 0.4. This study marked the first verification of the focusing schlieren technique in a major subsonic/transonic wind tunnel, and the first time that high quality, detailed pictures of high-Reynolds number flows were obtained in a cryogenic wind tunnel. This test was part of a development program to implement instrumentation techniques in cryogenic wind tunnels, with the ultimate aim to use them in the National Transonic Facility (NTF).
Aerodynamic investigation with focusing schlieren in a cryogenic wind tunnel
AIAA, Applied Aerodynamics Conference ; 1993 ; Monterey, CA, United States
1993-08-01
Conference paper
No indication
English
Aerodynamic investigation with focusing schlieren in a cryogenic wind tunnel
Tema Archive | 1994
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